Engineer Engineering
Resume:
E.JAGADEESH KUMAR
E-Mail: ************@*****.***
Contact: +91-994*******
EXPERIENCE SUMMARY
* ***** ** ********** ** Aerospace Design and Manufacturing Industry.
Current role is Engineer in Maini Global Aerospace.
1. Company : Honeywell Aerospace and Quest Global.
Designation : Senior Engineer.
2. Company : Maini Precision Products Ltd.
Designation : Engineer.
3. Company : Ravilla Aerospace Industries Pvt Ltd.
Designation : Design Engineer.
TECHNICAL SUMMARY
Autocad : 2D Sketch.
SolidWorks : Part modeling, Drafting, Assembly and Surface Modeling.
Catia V5 & V6 : Part modeling, Drafting, Assembly, Surface Modeling and
CNC Program generation.
Uni Graphics : Part modeling, Drafting, Assembly and CNC Program generation.
ACADEMIC QUALIFICATION
2008 – 2012 : BE-Aeronautical Engineering - Karpagam Institute of Tech with 75%
University : Anna University, India.
TECHNICAL DOCUMENTATION
Range Increment of smart bombs (Joint Direct Attack Munition) by using external retractable gliding wings.
PROFESSIONAL EXPOSURE
Design and Manufacturing of Aerospace and Automobile components.
CNC CAM programming.
Designing of Jigs and Fixtures.
Failiure Mode Effective Analysis.
Cycle time reduction.
Knowledge in Geometric Dimensioning and Tolerance.
Well versed with AS9100 REV C QMS Documentation.
Selection tools like solid & insert type cutter for machining materials like Inconel, Magnesium and Titanium
Knowledge in special process like anodizing, passivation and yellow chrome platting.
Knowledge in Non Destructive Testing.
Knowledge in Honning, Cylindrical grinding and surface grinding process.
Understanding of ASME Y14.5 and other technical Standards.
KAIZEN in engineering process and implementation.
Using of SAP ERP, Teamcenter and Aerolean.
PROJECT DETAILS
LEAP ENGINE –SNECMA SAFRAN
Description:
The LEAP means Leading Edge Aviation Propulsion. It is a high BYPASS Turbofan Engine.It is currently under development by CFM International, a 50-50 joint venture company between GE Aviation of the United States and Snecma of France. Major applications of this engine are Airbus A320, Boing 737 MAX and COMAC C919.
Responsibilities:
Involved in process planning team member for manufacture.
Involved in Fixture Designing and NC program by using Catia.
Involved in implementing manufacturing process .
Involved in engineering documentations.
BELL CRANK PROJECT-GENERAL ELECTRIC
Description:
Bell crank is a high precision steel alloy casting and its assembly pin which are the
parts used in vane actuations in all GE Engines.
Responsibilities:
Involved in process planning team member for manufacture.
Design of Jigs. Fixtures and NC program by using catia.
Handling of engineering documentations.
BOEING TEST AND EVALUATION
Description:
Structural frames are some of parts which is made of aluminum alloys and assembly by using rivets and Nut plates.
Responsibilities:
Involved in process planning for manufacture.
Design and implementation of Jigs and Fixtures by using autocad and catia.
Creating model and NC program for manufacturing .
WING ASSEMBLY –Vikram Sarabhai Space Center
Description:
Rudder Shafts, Ribs, Front & Rear Spars, Leading & Trailing edges are all Assembled in wings for Reusable Launch Vehicle/Technology Demonstrator.
Responsibilities:
Involved in process planning team member for manufacture.
Conversion of 2D drawings into 3D models to creat NC program.
Design and Implementation of Jigs and Fixtures by using solidworks.
Involved in engineering documentations.
GEARBOX ASSEMBLY- HINDUSTAN AERONAUTICS LTD
Description:
Main Gearbox Housing is a magnisium alloy material which is used to assemble the Rotors Blade for Dhruv Helicopters and Covers & Flange is a Inconel material used in Sukhoi Aircraft Engines.
Responsibilities:
Involved in process planning team member for manufacture.
Conversion of 2D drawings into 3D models to create NC program.
Design and implementation of Jigs and Fixtures by using solidworks.
Analyse and fix the production issue.
Handling of engineering documentations.
MISSILE FRAMES – GODREJ & BOYCE
Description:
Frames are all Aluminium alloy material which is used in Brahmos missile for Naval application. Canister body is Titanium material which is used in exhaust section of Brahmos missile and Cylinders which is made of steel, used in akash missile.
Responsibilities:
Involved in process planning team member for manufacture.
Design and implementation of Jigs and Fixtures by using catia.
Handling of engineering documentations.
Vendor follow up for special process.
PERSONAL DETAILS
Date of Birth : 12-09-1989
Sex : Male
Parent’s Name : Mr. K.G.Eswaramoorthi, Mrs E.Selvi
Martial Status : Single
Permanent Address : 2/121,Goundampalayam,Peruntholuvu(po),
Tiruppur-641665,
Tamil nadu, India
Passport Number : K0401556
I hereby declare that all the above information is true to the best of my knowledge.
Date : Authentically
Place : Bangalore. E.Jagadeesh Kumar.
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